A joint NASA/Boeing team has completed the first phase of flight tests on the unique X-48B Blended Wing Body aircraft at NASA's Dryden Flight Research Center on Edwards Air Force Base, Calif. The team completed the 80th and last flight of the project's first phase on March 19, 2010. (NASA photo / Tony Landis) EDWARDS, Calif. - A team led by NASA and The Boeing Company has completed the first phase of flight tests on the subscale X-48B blended wing body aircraft at the agency's Dryden Flight Research Center in Edwards, Calif.

The remotely piloted, 500-pound airplane with the silhouette resembling a manta ray – also called a hybrid wing body - is a tool of NASA's new Environmentally Responsible Aviation, or ERA, Project, which aims to develop the technology needed to create a quieter, cleaner, and more fuel-efficient airplane for the future.

A flying test bed such as the X-48B enables NASA to assess and validate the key technologies. The recently concluded flight tests ascertained the handling and flying qualities of such an aircraft at speeds typical of landings and takeoffs.

"This project is a huge success," said Fay Collier, manager of the ERA Project in NASA's Aeronautics Research Mission Directorate. "Bottom line: the team has proven the ability to fly tailless aircraft to the edge of the low-speed envelope safely."

Until recently, Collier was principal investigator for NASA's Subsonic Fixed Wing Project, which established the partnership with Boeing to conduct initial, fundamental technology development efforts with the X-48B. The ERA Project he now leads is part of a new research program NASA initiated to help further mature promising technology before transfer to industry.

The team completed the 80th and last flight of the project's first phase on March 19, 2010, almost three years after the X-48B's first flight on July 20, 2007.

Cranfield Aerospace Limited technician Ian Brooks prepares the X-48B for flight. (NASA photo / Tony Landis) In addition to NASA and Boeing, the team includes Cranfield Aerospace Limited of the United Kingdom, and the U.S. Air Force Research Laboratory of Dayton, Ohio.

In the mid-2000s, NASA identified low-speed flight controls as a development challenge for aircraft such as the hybrid wing body. This challenge, and the challenge of building a non-circular, pressurized fuselage structure, have been the initial focuses of research since then. The ultimate goal is to develop technology for an environmentally friendly aircraft that makes less noise, burns less fuel, and emits less noxious exhaust.

The milestones accomplished by the team focused on three main technical objectives: flight envelope expansion, aircraft performance characterization, and validation of flight control software limiters.

The first objective, envelope expansion, consisted of 20 flights over a year-long period. For these flights, the aircraft was flown through a variety of maneuvers intended to define the overall flight capabilities and discern the general stability and handling characteristics of the aircraft. Completion of these tests resulted in a preliminary flight envelope adequate for transition to higher risk testing.

The second objective, aircraft performance characterization, focused on stall testing to define the boundaries of controlled flight, engine-out maneuvering to understand how to control the aircraft if one or more engines malfunctioned, and parameter identification flights to evaluate how movements of flight control surfaces affected the airplane's performance.

NASA Dryden engineer Gary Cosentino prepares the X-48B for flight. (NASA photo / Tony Landis) In 52 flights from July 2008 through December 2009, engineers quantified the dynamic response of the aircraft by sending computer commands to the X-48B's flight control surfaces and measuring how quickly the plane responded to the inputs.

The third and most important objective were limiter assaults, in which the remote pilot deliberately exceeded the defined boundaries of controllability – such as angle of attack, sideslip angle and acceleration - to see whether the airplane's computer could keep it flying steady. Eight flight tests validated the programmed limiters and gave the team confidence that a robust, versatile, and safe control system could be developed for such an aircraft.

Tests with the X-48B will continue later this year, after a new flight computer is installed and checked out. The next series of flight tests will focus on additional parameter identification investigations.

NASA has a second hybrid wing body aircraft, the X-48C, which it has modified for a noise profile even lower than the X-48B's, and is preparing for test flights to investigate other controllability factors.

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PHOTO EDITORS: High-resolution photos to support this release are available electronically on the NASA Dryden web site at: